US10589353B2 - Datum structure for additively manufactured object removal from build platform - Google Patents

Abstract

An additively manufactured (AM) structure includes a removal plane extending therein defining an object thereabove. The AM structure also includes at least one datum structure coupled relative to the AM structure. Each datum structure includes a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure through the removal plane. The vertical reference plane is horizontally coplanar with the removal plane of the AM structure. The datum structures allow for accurate object cuts regardless of whether an AM build platform is horizontal or non-planar.

Description

BACKGROUND OF THE INVENTION

The disclosure relates generally to additive manufacturing (AM), and more particularly, to a datum structure for use in guiding removal of an object from an AM structure, which may be on an upper surface of an AM build platform.

The pace of change and improvement in the realms of power generation, aviation, and other fields has accompanied extensive research for manufacturing objects used in these fields. Conventional manufacture of metallic, plastic or ceramic composite objects generally includes milling or cutting away regions from a slab of material before treating and modifying the cut material to yield a part, which may have been simulated using computer models, e.g., in drafting software. Manufactured objects which may be formed from metal can include, e.g., airfoil objects for installation in a turbomachine such as an aircraft engine or power generation system.

Additive manufacturing (AM) includes a wide variety of processes of producing an object through the successive layering of material rather than the removal of material. As such, additive manufacturing can create complex geometries without the use of any sort of systems, molds or fixtures, and with little or no waste material. Instead of machining objects from solid billets of material, much of which is cut away and discarded, the only material used in additive manufacturing is what is required to shape the object.

Additive manufacturing techniques typically include taking a three-dimensional computer aided design (CAD) file of the object to be formed, electronically slicing the object into layers, e.g., 18-102 micrometers thick, and creating a file with a two-dimensional image of each layer, including vectors, images or coordinates. The file may then be loaded into a preparation software system that interprets the file such that the object can be built by different types of additive manufacturing systems. In 3D printing, rapid prototyping (RP), and direct digital manufacturing (DDM) forms of additive manufacturing, material layers are selectively dispensed, sintered, formed, deposited, etc., to create the object.

In metal powder additive manufacturing techniques, such as direct metal laser melting (DMLM) (also referred to as selective laser melting (SLM)), metal powder layers are sequentially melted together to form an additive manufacturing (AM) structure that includes the object. More specifically, fine metal powder layers are sequentially melted after being uniformly distributed using an applicator on a metal powder bed. Each applicator includes an applicator element in the form of a lip, brush, blade or roller made of metal, plastic, ceramic, carbon fibers or rubber that spreads the metal powder evenly over the build platform. The metal powder bed can be moved in a vertical axis. The process takes place in a processing chamber having a precisely controlled atmosphere. Once each layer is created, each two dimensional slice of the object geometry can be fused by selectively melting the metal powder. The melting may be performed by a high powered melting beam, such as a 100 Watt ytterbium laser, to fully weld (melt) the metal powder to form a solid metal. The melting beam moves in the X-Y direction using scanning mirrors, and has an intensity sufficient to fully weld (melt) the metal powder to form a solid metal. The metal powder bed may be lowered for each subsequent two dimensional layer, and the process repeats until the AM structure is completely formed. Once the AM structure is complete, at least a portion thereof can be removed from the build platform, creating the final object. In order to create certain larger objects faster, some metal additive manufacturing systems employ more than one high powered laser that work together to form a larger AM structure including the larger object.

Build platforms used in metal powder additive manufacturing typically have a number of desirable attributes. First, an upper surface of the build platform should be installed in horizontal alignment with an applicator of the AM system to ensure even layers of raw material are created.FIG. 1 shows abuild platform10 and itsupper surface12 in a horizontal or non-tilted position, i.e., aligned with an applicator element (not shown). During additive manufacturing, additive manufacturing (AM)structures14A-C are sequentially built onupper surface12. EachAM structure14A-C includes aportion16A-C therein configured to be anobject18A-C after the object is cut from anyremaining portion20A-C of the AM structure onupper surface12. More specifically, eachAM structure14A-C includes aremoval plane22A-C extending therein defining anobject18A-C thereabove. Ideally,build platform10 is horizontal such thatremoval planes22A-C are coplanar, and equidistant fromupper surface12 after being formed. That is,build platform10 is horizontally aligned with the applicator element of the AM system (not shown) so even layers of raw material are created. In this case, a cutting element (not shown)(e.g., that of a wire electrical discharge machine (w-EDM)) would remove eachobject18A-E from aremaining portion20A-C ofAM structure14A-C by cutting parallel toupper surface12 throughremoval planes22A-C, along the dashed line. This process uses zero point clamping devices (not shown) to employupper surface12 as a vertical reference plane (not the objects) for guiding the cutting element. Referring toFIG. 2, wherebuild platform10 is not horizontal in the AM system, the AM system naturally enlargesportions20A-C during the build ofAM structures14A-C such thatobjects18A-C all extend to the same height. Here, whenupper surface12 acts as a vertical reference plane for guiding the cutting element, eachobject18A-C is not cut off near the desired final dimensions during the w-EDM process.

A second desirable attribute of a build platform is that it be planar. Build platforms can become non-planar in a number of ways. First, as shown inFIG. 3, during additive manufacturing, build platforms may deform, e.g., due to thermal stress, or the weight ofobjects14A-E thereon. Second, build platforms are typically machined between reuses to, for example, remove remaining portions (e.g.,22A-C inFIG. 2) of AM structures. The machining can result in non-planar upper surfaces on the build platform. As shown inFIG. 3, whenupper surface12 acts as a vertical reference plane for guiding the cutting element and it is not planar, eachobject14A-E is not cut off near the desired final dimensions during the w-EDM process.

Regardless of whether the build platform is not horizontal or not planar, each resulting object must be extensively machined to remove the unwanted material, which increases cost and time necessary to manufacture each object. The unwanted material oftentimes ends up as waste, diminishing the benefits of the additive manufacturing process.

BRIEF DESCRIPTION OF THE INVENTION

A first aspect of the disclosure provides an apparatus, comprising: a build platform configured to support an object build in an additive manufacturing system, the build platform having an upper surface being at least one of non-horizontal and non-planar; an additively manufactured (AM) structure on the upper surface of the build platform, the AM structure including a removal plane extending therein defining an object thereabove; and a datum structure positioned relative to the build platform and including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure, the vertical reference plane horizontally coplanar with the removal plane.

A second aspect of the disclosure provides a method, comprising: additively manufacturing at least one additive manufacturing (AM) structure on an upper surface of a build platform, the upper surface being at least one of non-horizontal and non-planar, each AM structure including a removal plane extending therein defining an object thereabove; and while additively manufacturing the at least one AM structure, additively manufacturing at least one datum structure positioned relative to the build platform, each datum structure including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure, wherein each vertical reference plane is horizontally coplanar with the removal plane of each AM structure.

A third aspect of the disclosure provides an additively manufactured (AM) structure, comprising: a removal plane extending therein defining an object thereabove; and at least one datum structure coupled relative to the AM structure, the at least one datum structure including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure on the build platform through the removal plane, the vertical reference plane horizontally coplanar with the removal plane of the object.

The illustrative aspects of the present disclosure are designed to solve the problems herein described and/or other problems not discussed.

BRIEF DESCRIPTION OF THE DRAWINGS

These and other features of this disclosure will be more readily understood from the following detailed description of the various aspects of the disclosure taken in conjunction with the accompanying drawings that depict various embodiments of the disclosure, in which:

FIG. 1 shows a side view of a conventional horizontal and planar build platform with AM structures thereon.

FIG. 2 shows a side view of a conventional non-horizontal build platform with AM structures thereon.

FIG. 3 shows a side view of a conventional non-planar build platform with AM structures thereon.

FIG. 4 shows a block diagram of an additive manufacturing system and process including a non-transitory computer readable storage medium storing code representative of an AM structure according to embodiments of the disclosure.

FIG. 5 shows a schematic perspective view of a two melting beam source additive manufacturing system building an object.

FIG. 6 shows a schematic plan view of respective fields of a four melting beam source additive manufacturing system.

FIG. 7 shows a perspective view of a non-horizontal build platform having additive manufacturing (AM) structures including datum structures according to embodiments of the disclosure.

FIG. 8 shows a side view of the non-horizontal build platform ofFIG. 7.

FIG. 9 shows a side view of a non-planar build platform having additive manufacturing (AM) structures including datum structures according to embodiments of the disclosure.

FIG. 10 shows a side view of an additive manufactured (AM) structures including datum structures thereon according to embodiments of the disclosure.

FIG. 11 shows a side view of a build platform having additive manufacturing (AM) structures including datum structures on a sacrificial support according to embodiments of the disclosure.

FIG. 12 shows a side view of a non-planar build platform having additive manufacturing (AM) structures including different pluralities of datum structures according to embodiments of the disclosure.

It is noted that the drawings of the disclosure are not to scale. The drawings are intended to depict only typical aspects of the disclosure, and therefore should not be considered as limiting the scope of the disclosure. In the drawings, like numbering represents like elements between the drawings.

DETAILED DESCRIPTION OF THE INVENTION

Embodiments of the disclosure provide an apparatus, method and additive manufactured (AM) structure that employ a datum structure including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure. The datum structure may be positioned relative to a build platform or the AM structure. The build platform is configured to support an object build in an additive manufacturing system, and has an upper surface that is non-horizontal and/or non-planar. An AM structure is additively manufactured on the upper surface of the build platform, and includes a removal plane extending therein defining an object, i.e., a final product of the AM, thereabove. Cutting through the removal plane results in the object being near its desired final dimensions. The datum structure provides a vertical reference plane that is horizontally coplanar with the removal plane. In this manner, a cutting element used to remove the object from the AM structure can reference the vertical reference plane of the datum structure, rather than the upper surface of the build platform, so the objects are cut off in a uniform manner and near the desired final dimensions. The disclosure thus reduces the need to be exact in positioning the build platform horizontal, e.g., aligned with the applicator, in the AM system, and reduces the need for the build platform to be perfectly planar. The datum structures also improve the precision and speed of cut, e.g., using wire electrical discharge machining (w-EDM), and separation of objects from a remaining portion of the AM structure.

FIG. 4 shows a schematic/block view of an illustrative computerized metal powder additive manufacturing system100 (hereinafter ‘AM system100’) for generating an AM structure(s)102. The term “AM structure” is used herein to describe that structure built by the AM process inAM system100 that includes a final object but also perhaps some remaining portion that needs to be removed to arrive at the final object. The remaining portion may remain on a build platform of the AM system or be cut away from the AM structure after it is removed from the build platform. Each AM structure includes a removal plane extending therein defining an object thereabove. Each “object” represents the final or near final product of the AM process (perhaps with some finishing thereafter). One large AM structure or multiple AM structures, e.g., twoAM structures102A,102B as shown, may be created at one time (only a single layer thereof is shown). The teachings of the disclosures will be described relative to building AM structure(s)102 using multiple melting beam sources, e.g., fourlasers110,112,114,116, but it is emphasized and will be readily recognized that the teachings of the disclosure are equally applicable to build multiple AM structure(s)102 using any number of melting beam sources, i.e., one or more. In this example,AM system100 is arranged for direct metal laser melting (DMLM). It is understood that the general teachings of the disclosure are equally applicable to other forms of metal powder additive manufacturing such as but not limited to direct metal laser sintering (DMLS), selective laser sintering (SLS), electron beam melting (EBM), and perhaps other forms of additive manufacturing. AM structure(s)102 are illustrated as circular elements to create circular objects; however, it is understood that the additive manufacturing process can be readily adapted to manufacture any shaped object, a large variety of objects and a large number of objects on abuild platform118.

AM system100 generally includes a metal powder additive manufacturing control system120 (“control system”) and anAM printer122. As will be described,control system120 executes object code124O to generate AM structure(s)102 using multiplemelting beam sources110,112,114,116. In the example shown, four melting beam sources may include four lasers. However, the teachings of the disclosures are applicable to any melting beam source, e.g., an electron beam, laser, etc.Control system120 is shown implemented oncomputer126 as computer program code. To this extent,computer126 is shown including amemory130 and/orstorage system132, a processor unit (PU)134, an input/output (110)interface136, and abus138. Further,computer126 is shown in communication with an external110 device/resource140 andstorage system132. In general, processor unit (PU)134 executescomputer program code124 that is stored inmemory130 and/orstorage system132. While executingcomputer program code124, processor unit (PU)134 can read and/or write data to/frommemory130,storage system132, I/O device140 and/orAM printer122.Bus138 provides a communication link between each of the components incomputer126, and I/O device140 can comprise any device that enables a user to interact with computer126 (e.g., keyboard, pointing device, display, etc.).Computer126 is only representative of various possible combinations of hardware and software. For example, processor unit (PU)134 may comprise a single processing unit, or be distributed across one or more processing units in one or more locations, e.g., on a client and server. Similarly,memory130 and/orstorage system132 may reside at one or more physical locations.Memory130 and/orstorage system132 can comprise any combination of various types of non-transitory computer readable storage medium including magnetic media, optical media, random access memory (RAM), read only memory (ROM), etc.Computer126 can comprise any type of computing device such as an industrial controller, a network server, a desktop computer, a laptop, a handheld device, etc.

As noted,AM system100 and, inparticular control system120, executesprogram code124 to generate AM structure(s)102 (eventually, objects).Program code124 can include, inter alia, a set of computer-executable instructions (herein referred to as ‘system code124S’) foroperating AM printer122 or other system parts, and a set of computer-executable instructions (herein referred to as ‘object code124O’) defining AM structure(s)102 (and the object to be therein) to be physically generated byAM printer122. As described herein, additive manufacturing processes begin with a non-transitory computer readable storage medium (e.g.,memory130,storage system132, etc.)storing program code124.System code124S for operatingAM printer122 may include any now known or later developed software code capable of operatingAM printer122.

Object code124O defining AM structure(s)102 may include a precisely defined 3D model of an object and any other necessary supporting structures (e.g., a remaining portion ofAM structure102 or a sacrificial support). Object code124O can be generated from any of a large variety of well-known computer aided design (CAD) software systems such as AutoCAD®, TurboCAD®, DesignCAD 3D Max, etc. In this regard, object code124O can include any now known or later developed file format. Furthermore, object code124O representative of AM structure(s)102 may be translated between different formats. For example, object code124O may include Standard Tessellation Language (STL) files which was created for stereolithography CAD programs of 3D Systems, or an additive manufacturing file (AMF), which is an American Society of Mechanical Engineers (ASME) standard that is an extensible markup-language (XML) based format designed to allow any CAD software to describe the shape and composition of any three-dimensional object to be fabricated on any AM printer. Object code124O representative of AM structure(s)102 may also be converted into a set of data signals and transmitted, received as a set of data signals and converted to code, stored, etc., as necessary. In any event, object code124O may be an input toAM system100 and may come from a part designer, an intellectual property (IP) provider, a design company, the operator or owner ofAM system100, or from other sources. In any event,control system120 executessystem code124S and object code124O, dividing AM structure(s)102 into a series of thin slices that assembles usingAM printer122 in successive layers of material.

AM printer122 may include aprocessing chamber142 that is sealed to provide a controlled atmosphere for AM structure(s)102 printing, e.g., a set pressure and temperature for lasers, or a vacuum for electron beam melting. Abuild platform118, upon which AM structure(s)102 is/are built, is positioned withinprocessing chamber142. As will be described herein, mountingbuild platform118 in a horizontal manner, e.g., such that it is aligned with applicator164 (described elsewhere herein) can be challenging. Further,build platform118 may include anupper surface119 that is not planar. In any event, a number ofmelting beam sources110,112,114,116 are configured to melt layers of metal powder onbuild platform118 to generate AM structure(s)102. While fourmelting beam sources110,112,114,116 will be described herein, it is emphasized that the teachings of the disclosure are applicable to a system employing any number of sources, e.g., 1, 2, 3, or 5 or more.

FIG. 5 shows a schematic perspective view of melting beams of AM system using twomelting beam sources110,112, e.g., lasers. During operation, the melting beam(s) (dashed lines) are guided, e.g., by scanner mirrors for lasers or electromagnetic field/electric coils for electron beams, along scan vectors (paths), which are indicated by arrows on a top surface ofillustrative object200.Internal scan vectors202 meltinner regions204 ofobject200 that scan linearly across a layer, and a verythin border206 is melted with one to threecontour scan vectors208 that only follow a desired outer edge of the layer. Eachlaser110,112 has its own field (1 and 2, respectively) upon which it can work. Eachmelting beam source110,112 may work within only a small portion of its respective field at any given time. Each field and the scan vectors are assigned to one or theother source110,112 with an interface210 (within circle) wherefields1,2 of pair ofsources110,112 meet. Which scan vector is made by which source usually depends on the region that can be reached by each source. Eachmelting beam source110,112 is calibrated in any now known or later developed manner. That is, eachmelting beam source110,112 has had its laser or electron beam's anticipated position relative to buildplatform118 correlated with its actual position in order to provide an individual position correction (not shown) to ensure its individual accuracy.Interface210 inbody222 ofAM structure200 defines afirst portion224 and asecond portion226 ofbody222 of an object made by differentmelting beam sources110,112 of multiple melting beamsource AM system100 during a single build. Here, fields1,2 meet at a line, creating aplanar interface228 inobject200.

FIG. 6 shows a schematic plan view of melting beams of AM system using fourmelting beam sources110,112,114,116, e.g., lasers. Eachmelting beam source110,112,114,116 has afield1,2,3 or4 including anon-overlapping field region230,232,234,236, respectively, in which it can exclusively melt metal powder, and at least one overlapping field region or interfaces240,242,244,246 in which two or more sources can melt metal powder. (Boxed numbers ofsources110,112,114,116 indicate which source creates the shape illustrated thereabout). In this regard, eachmelting beam source110,112,114,116 may generate a melting beam (two shown,160,162, inFIG. 1), respectively, that fuses particles for each slice, as defined by object code124O. For example, inFIG. 4,melting beam source110 is shown creating a layer ofAM structure102 usingmelting beam160 in one region, while meltingbeam source112 is shown creating a layer ofAM structure102 usingmelting beam162 in another region. Eachmelting beam source110,112,114,116 is calibrated in any now known or later developed manner. That is, eachmelting beam source110,112,114,116 has had its laser or electron beam's anticipated position relative to buildplatform118 correlated with its actual position in order to provide an individual position correction (not shown) to ensure its individual accuracy. In one embodiment, each of pluralitymelting beam sources110,112,114,116 may create melting beams, e.g.,160,162 (FIG. 4), having the same cross-sectional dimensions (e.g., shape and size in operation), power and scan speed. It is recognized that while foursources110,112,114,116 have been illustrated to describe an interface for overlapping fields, any two sources may create overlapping fields.

Returning toFIG. 4, anapplicator164 may create a thin, even layer ofraw material166 spread out as the blank canvas from which each successive slice of the final object will be created. However, as described in more detail herein, wherebuild platform118 is not horizontal or not planar, layer ofraw material166 is not evenly distributed, resulting in AM structures having removal planes for objects therein that are at different distances fromupper surface119 of build platform118 (see e.g.,FIGS. 2 and 3).Applicator164 may move under control of alinear transport system168.Linear transport system168 may include any now known or later developed arrangement for movingapplicator164. In one embodiment,linear transport system168 may include a pair of opposingrails170,172 extending on opposing sides ofbuild platform118, and alinear actuator174 such as an electric motor coupled toapplicator164 for moving it along rails170,172.Linear actuator174 is controlled bycontrol system120 to moveapplicator164. Other forms of linear transport systems may also be employed.Applicator164 take a variety of forms. In one embodiment,applicator164 may include abody176 configured to move along opposingrails170,172, and an actuator element (not shown inFIG. 4) in the form of a tip, blade or brush configured to spread metal powder evenly overbuild platform118, i.e.,build platform118 or a previously formed layer of AM structure(s)102, to create a layer of raw material. The actuator element may be coupled tobody176 using a holder (not shown) in any number of ways. The process may use different raw materials in the form of metal powder. Raw materials may be provided toapplicator164 in a number of ways. In one embodiment, shown inFIG. 4, a stock of raw material may be held in araw material source178 in the form of a chamber accessible byapplicator164. In other arrangements, raw material may be delivered throughapplicator164, e.g., throughbody176 in front of its applicator element and overbuild platform118. In any event, anoverflow chamber179 may be provided on a far side ofapplicator164 to capture any overflow of raw material not layered onbuild platform118. InFIG. 4, only oneapplicator164 is shown. In some embodiments,applicator164 may be among a plurality of applicators in which applicator164 is an active applicator and other replacement applicators (not shown) are stored for use withlinear transport system168. Used applicators (not shown) may also be stored after they are no longer usable.

In one embodiment, AM structure(s)102 may be made of a metal which may include a pure metal or an alloy. In one example, the metal may include practically any non-reactive metal powder, i.e., non-explosive or non-conductive powder, such as but not limited to: a cobalt chromium molybdenum (CoCrMo) alloy, stainless steel, an austenite nickel-chromium based alloy such as a nickel-chromium-molybdenum-niobium alloy (NiCrMoNb) (e.g., Inconel 625 or Inconel 718), a nickel-chromium-iron-molybdenum alloy (NiCrFeMo) (e.g., Hastelloy® X available from Haynes International, Inc.), or a nickel-chromium-cobalt-molybdenum alloy (NiCrCoMo) (e.g., Haynes 282 available from Haynes International, Inc.), etc. In another example, the metal may include practically any metal such as but not limited to: system steel (e.g., H13), titanium alloy (e.g., Ti6Al4V), stainless steel (e.g., 316L) cobalt-chrome alloy (e.g., CoCrMo), and aluminum alloy (e.g., AlSi₁₀Mg). As will be described herein, datum structure(s) according to embodiments of the disclosure may be made from the same materials as AM structure(s)102.

The atmosphere withinprocessing chamber142 is controlled for the particular type of melting beam source being used. For example, for lasers,processing chamber142 may be filled with an inert gas such as argon or nitrogen and controlled to minimize or eliminate oxygen. Here,control system120 is configured to control a flow of aninert gas mixture180 withinprocessing chamber142 from a source ofinert gas182. In this case,control system120 may control apump184, and/or aflow valve system186 for inert gas to control the content ofgas mixture180.Flow valve system186 may include one or more computer controllable valves, flow sensors, temperature sensors, pressure sensors, etc., capable of precisely controlling flow of the particular gas. Pump184 may be provided with or withoutvalve system186. Where pump184 is omitted, inert gas may simply enter a conduit or manifold prior to introduction toprocessing chamber142. Source ofinert gas182 may take the form of any conventional source for the material contained therein, e.g. a tank, reservoir or other source. Any sensors (not shown) required to measuregas mixture180 may be provided.Gas mixture180 may be filtered using afilter188 in a conventional manner. Alternatively, for electron beams,processing chamber142 may be controlled to maintain a vacuum. Here,control system120 may control apump184 to maintain the vacuum, and flowvalve system186, source ofinert gas182 and/or filter188 may be omitted. Any sensors (not shown) necessary to maintain the vacuum may be employed.

Avertical adjustment system190 may be provided to vertically adjust a position of various parts ofAM printer122 to accommodate the addition of each new layer, e.g., abuild platform118 may lower and/orchamber142 and/orapplicator164 may rise after each layer.Vertical adjustment system190 may include any now known or later developed linear actuators to provide such adjustment that are under the control ofcontrol system120.

In operation, buildplatform118 with metal powder thereon is provided withinprocessing chamber142, andcontrol system120 controls the atmosphere withinprocessing chamber142.Control system120 also controlsAM printer122, and in particular, applicator164 (e.g., linear actuator174) and melting beam source(s)110,112,114,116 to sequentially melt layers of metal powder onbuild platform118 to generate AM structure(s)102,200 (hereinafter just referenced with102) according to embodiments of the disclosure. As noted, various parts ofAM printer122 may vertically move viavertical adjustment system190 to accommodate the addition of each new layer, e.g., abuild platform118 may lower and/orchamber142 and/orapplicator164 may rise after each layer.

Referring toFIGS. 7-12, embodiments of the disclosure address the situation wherebuild platform118 is not horizontal inAM system100, or includes anupper surface119 that is not planar (see e.g.,FIGS. 2 and 3).

Referring initially toFIGS. 7-9,FIG. 7 shows a perspective view of abuild platform118 having AM structure(s)102 thereon, andFIGS. 8 and 9 show side views of twodifferent build platforms118 with AM structure(s)102 thereon. In theFIGS. 7 and 8 examples,build platform118 is not horizontal, e.g., it is not mounted horizontally aligned with applicator164 (FIG. 4) of AM system100 (FIG. 4) and/or it is slanted, tilted, etc. As a result,AM structures102 have different heights relative toupper surface119 ofbuild platform118.FIG. 9 shows another embodiment ofbuild platform118 where it is not planar, e.g., it is curved and/or has raised or lowered areas, etc.Build platform118 may be non-planar for a number of reasons. For example, it may deform during additive manufacturing, e.g., due to thermal stress, or the weight ofobjects14A-E thereon. Alternatively, it may be non-planar due to machining between uses.

A method according to embodiments of the disclosure includes additively manufacturing AM structure(s)102 onupper surface119 ofbuild platform118, i.e., in an AM system100 (FIG. 4). As described herein, eachAM structure102 may include aremoval plane314 extending therein defining anobject306 thereabove. That is,removal plane314 defines a lowermost extent ofobject306. AM structure102 (FIGS. 8 and 9) is configured to haveobject306 created therefrom by the object being cut away from a remaining portion312 (FIGS. 8 and 9) ofAM structure102. That is,removal plane314 represents a plane that whenobject306 is cut away from remainingportion312,object306 is at or near its final dimensions. As used herein, “near” indicates only minor finishing work is required to finalizeobject306 dimensions. Whileremoval plane314 is illustrated herein as a non-curved plane, it is understood that some deviation from perfectly planar, e.g., curvature, dips, verticality, etc., may be created during cutting ofobject306 from remainingportion312, e.g., within outer sides ofobject306 and where the cuttingelement304 allows. Here,datum structures300 at the very least indicate the entry and exit planes at which cuttingelement304 must enter and exitAM structure102. As will be described, remainingportion312 may remain onupper surface119 ofbuild platform118 whereobject306 is cut away therefrom, or it may be cut away fromAM structure102 after theAM structure102 is removed frombuild platform118.

While AM structure(s)102 are being additively manufactured, in contrast to conventional processes,AM system100 also additively manufactures at least onedatum structure300. In one embodiment, where object(s)306 will be cut away frombuild platform118, datum structure(s)300 may be positioned relative to buildplatform118. As noted, eachdatum structure300 includes vertical reference plane302 (FIGS. 8 and 9) for guidingcutting element304 to remove theobject306 from remainingportion312 ofobject306. As observed best inFIGS. 8 and 9, eachvertical reference plane302 is horizontally coplanar withremoval plane314 of eachobject306. In this fashion, cuttingelement304 can simply use vertical reference plane(s)302 as a guide to cut object(s)306 at or near their desired, final dimensions. Datum structure(s)300 may have any horizontal cross-sectional shape desired, and may be defined in object code124O along with the rest ofAM structure102.

A height to which eachdatum structure300 is built may be defined in a number of ways. In one embodiment, eachdatum structure300 is defined in object code124O to build until its respectivevertical reference plane302 is coplanar with a known level ofremoval plane314 of eachAM structure102. In this regard, the height ofremoval plane314 is predetermined in object code124O based on object(s)306 to be built.

In any event, as shown inFIGS. 8 and 9, datum structure(s)300 are built along with AM structure(s)102 in such a way that they have different heights depending on where they are onbuild platform118, but they all have the samevertical reference plane302, i.e., upper surface, coplanar withremoval plane314. For example, inFIG. 8,build platform118 is lower on the left then on the right. Here, datum structure300A, on the left, is taller than datum structure300B, on the right, because layers of raw material166 (FIG. 4) are not present at the location of datum structure300B until later in the build. In other words, since the left side ofbuild platform118 is lower, structures (AM structure102 or datum structure300) start to build there earlier than on the right side, resulting in structures on the left being taller than those on the right. InFIG. 9, datum structures300 (six) are provided between rows ofAM structures102. Here,datum structures300 may have varying heights acrossupper surface119 ofbuild platform118 depending on the severity of the non-planarity. For example, inFIG. 9,build platform118 is lowest inarea322 and higher to the left and the right, but to different degrees. Here, for example, datum structure300C, on the left, is shorter than datum structure300D and300E but taller than datum structure300H on the far right. Each datum structure300 (and AM structure102) starts to build whenever layers of raw material166 (FIG. 4) start to be distributed in an area in which they are assigned to be built, which can vary overupper surface119. In any event,datum structures300 extend fromupper surface119 to provide avertical reference plane302 coplanar withremoval plane314 of eachAM structure102.

As described herein and as shown for example inFIGS. 7-9, a plurality ofAM structures102 may be additively manufactured at one time. In this case, at least tworemoval planes314 thereof are at different distances fromupper surface119 ofbuild platform118, butvertical reference planes302 ofdatum structures300 are horizontally coplanar with the removal planes314 thereof to provide the vertical reference plane for guiding the cuttingelement304 to remove the object from the remaining portion of the object.

Another step of the method may include removing object(s)306 from remainingportion312 of AM structure(s)102. Cuttingelement304 can be any now known or later developed element configured to cut throughremoval plane314 to removeobjects306 from remainingportion312 of AM structure(s)102. In one embodiment, cuttingelement304 can be that of a wire electrical discharge machine (w-EDM). The “guiding” of cuttingelement304 by vertical reference plane(s)302 can take any form that ensure cuttingelement304 cuts through removal plane(s)314 in a uniform manner. In one example, cuttingelement304, e.g., of the w-EDM, passes parallel with eachvertical reference plane302, not cutting into it, and through eachremoval plane314 of eachobject310 to separate object(s)306. In another embodiment, cuttingelement304, e.g., of the w-EDM, may cut through a small predetermined, portion of eachvertical reference plane302 and through eachremoval plane314 of eachobject310 to separate object(s)306.

Datum structures300 can be positioned in a number of locations. In theFIGS. 7-9 embodiments, eachdatum structure300 is additively manufactured directly onupper surface119 ofbuild platform118 and separated fromAM structure102. In other embodiments, it may be advantageous to additively manufacture datum structure(s)300 coupled toAM structure102. For example,FIG. 10 shows a side view of anAM structure102 that has a relatively large size and may be additively manufactured, perhaps alone, onbuild platform118. In this case,AM structure102 may be removed from build platform before any remainingportion312 of AM structure requiring removal is removed.AM structure102 may be supported on another support such as a table. In this case, datum structure(s)300 may be additively manufactured as part ofAM structure102. Here,AM structure102 may includeremoval plane314 extending therein definingobject306 thereabove. That is,removal plane314 defines a lowermost extent ofobject306. In this embodiment, datum structure(s)300 may be coupled relative toAM structure102 such that cuttingelement304 can cut alongremoval plane314. In one embodiment, shown inFIG. 10, datum structure(s)300 may be coupled to AM structure(s)102, e.g., to remainingportion312. In another embodiment, shown inFIG. 11,AM structure102 may include any of a wide variety of sacrificial support(s)332 configured to support a section of thereof during additive manufacturing, and datum structure(s)300 may be coupled to sacrificial support(s)332. That is, additively manufacturing datum structure(s)300 includes additively manufacturing them operatively coupled tosacrificial support332.Sacrificial support332 is not ultimately part ofobject306. Datum structure(s)300 includevertical reference plane302 for cuttingelement304 to removeobject306 from remainingportion312 ofobject310. Cuttingelement304 can cut throughremoval plane314 usingvertical reference plane302 that is horizontally coplanar withremoval plane314 ofobject310, as previously described. In this embodiment,AM structure102 may still be on build platform118 (FIG. 11) or already separated therefrom (FIG. 10, on table). In the latter case, alower surface330 ofobject306 ofAM structure102 may not be planar, e.g., due to the weight of the part. Here,removal plane314 may be preconfigured to allow for removal of the non-planar lower surface330 (and perhaps other structure not necessary to object306), making the part planar on itslower surface330. Thereafter, any remaining portion ofsupport332 may be removed in a conventional manner.

The number ofdatum structures300 employed can be user selected, and may vary depending on any number of factors such as but not limited to: number of objects being built; size, dimensions of objects; type of cutting element; size of build platform, etc. For example, inFIG. 7, three datum structures (1 hidden) are shown; inFIG. 8, twodatum structures300 are shown; and inFIG. 9, six are shown. According to embodiments of the disclosure, any number ofdatum structures300 can be employed. Where a plurality ofdatum structures300 are additively manufactured, they may be spaced in any manner desired, e.g., as shown inFIGS. 7 and 9. For example, they may be spaced aboutbuild platform118 or about AM structure(s)102. They may be placed, for example, at ends of rows ofAM structures102, at corners ofbuild platform118, between rows ofAM structures102, etc., or wherever necessary to allow guiding of cuttingelement304. Eachvertical reference plane314 of spaceddatum structures300 may be horizontally coplanar with othervertical reference planes314 of the rest of the spaced datum structures. In another embodiment, as shown inFIG. 12, where a plurality of spaceddatum structures300 are additively manufactured, they may be grouped. That is, they may be grouped into different pluralities of spaced datum structures, e.g.,300X,300Y,300Z, to address one or more AM structures, e.g.,102X,102Y,102Z, that are incapable or not desirable to cut all at one time. For example,AM structures102X,102Y,102Z may haveremoval planes314X,314Y,314Z, respectively, that are too vertically different, to be cut in a single cut even withdatum structures300 provided. Here, eachvertical reference plane302 of each plurality (or group) of datum structures may be horizontally coplanar with eachvertical reference plane302 of the rest of the same plurality (or group) of spaced datum structures, but not horizontally coplanar with the vertical reference planes of the other plurality(ies) (groups) of datum structures. For example,vertical reference planes302X of plurality ofdatum structures300X are horizontally coplanar with each other, but not horizontally coplanar withvertical reference planes302Y and/or302Z of the other plurality(ies) ofdatum structures300Y,300Z. The same can be said ofplanes302Y and302Z relative toplanes302X. In this example, a first cut (cut1) would removeAM structures102X throughremoval plane314X, a second cut (cut2) would removeAM structures102Y throughremoval plane314Y, and a third cut (cut3) would removeAM structures102Z throughremoval plane314Z. Any number of groups can be provided, each containing any number of AM structures102 (including just one).

Embodiments of the disclosure may include an intermediate apparatus400 (FIGS. 7-9, 11 and 12) includingbuild platform118 configured to support an object build inAM system100.Build platform118 hasupper surface119 that is non-horizontal and/or non-planar.Apparatus400 may include AM structure(s)102 onupper surface119 with eachAM structure102 includingremoval plane314 therein definingobject306 thereabove.Apparatus400 may also include datum structure(s)300 positioned relative to buildplatform118 and each includingvertical reference plane302 for guidingcutting element304 to remove the object from a remainingportion312 of the AM structure. As noted, eachvertical reference plane302 is horizontally coplanar with removal plane(s)314. Datum structure(s)300 may be onbuild platform118 separate from AM structure(s)102, coupled to AM structure(s) (separate from build platform), or coupled to a sacrificial support332 (FIG. 11).

In another embodiment, as shown inFIG. 10,AM structure102 includesremoval plane314 extending therein definingobject306 thereabove, and datum structure(s)300 coupled relative to the AM structure. Again, each datum structure(s)300 includesvertical reference plane302 for guidingcutting element304 to remove the object from a remainingportion312 of the AM structure throughremoval plane314, the vertical reference plane being horizontally coplanar with the removal plane of the object. As noted,lower surface330 ofAM structure102 may not be planar, e.g., after removal frombuild platform118.

Embodiments of the disclosure automatically compensate for errors in tilt of the build platform caused by, e.g., the initial leveling of the platform in the AM system. In addition, embodiments of the disclosure automatically compensate for errors in planarity of the build platform caused by, e.g., machining between uses. Where the cutting occurs from the build platform, using datum structure(s)300 provides improved accuracy compared to using the build platform itself for alignment as datum structure(s)200 automatically compensate for errors in the build platform. Where the cutting occurs after removal of the AM structure, datum structure(s)300 provide accurate cutting of unwanted portions thereof. Regardless of when the cut occurs, a precise vertical cut of height for the objects can be achieved despite build platform errors, enabling the cut to provide the final or near final desired object height and reducing any reworking of the objects. Shorter cycle times are also possible because the disclosure provides faster alignment of the build platform for object cut off. Further, the disclosure also reduces a scrap rate caused by cutting objects too short, and the amount of raw material stock required.

The foregoing drawings show some of the processing associated according to several embodiments of this disclosure. In this regard, each drawing or block within a flow diagram of the drawings represents a process associated with embodiments of the method described. It should also be noted that in some alternative implementations, the acts noted in the drawings or blocks may occur out of the order noted in the figure or, for example, may in fact be executed substantially concurrently or in the reverse order, depending upon the act involved. Also, one of ordinary skill in the art will recognize that additional blocks that describe the processing may be added.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or objects, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, objects, and/or groups thereof. “Optional” or “optionally” means that the subsequently described event or circumstance may or may not occur, and that the description includes instances where the event occurs and instances where it does not.

Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about,” “approximately” and “substantially,” are not to be limited to the precise value specified. In at least some instances, the approximating language may correspond to the precision of an instrument for measuring the value. Here and throughout the specification and claims, range limitations may be combined and/or interchanged, such ranges are identified and include all the sub-ranges contained therein unless context or language indicates otherwise. “Approximately” as applied to a particular value of a range applies to both values, and unless otherwise dependent on the precision of the instrument measuring the value, may indicate +/−10% of the stated value(s).

The corresponding structures, materials, acts, and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material, or act for performing the function in combination with other claimed elements as specifically claimed. The description of the present disclosure has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the disclosure in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the disclosure. The embodiment was chosen and described in order to best explain the principles of the disclosure and the practical application, and to enable others of ordinary skill in the art to understand the disclosure for various embodiments with various modifications as are suited to the particular use contemplated.

Claims (20)

What is claimed is:

1. An apparatus, comprising:

a build platform configured to support an object build in an additive manufacturing system, the build platform having an upper surface being at least one of non-horizontal and non-planar;

an additively manufactured (AM) structure on the upper surface of the build platform, the AM structure including a removal plane extending therein defining an object thereabove; and

a datum structure positioned relative to the build platform and including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure, the vertical reference plane horizontally coplanar with the removal plane.

2. The apparatus ofclaim 1, wherein the datum structure is directly on the build platform and separated from the AM structure.

3. The apparatus ofclaim 1, wherein the datum structure is coupled to the AM structure.

4. The apparatus ofclaim 1, wherein the AM structure further includes a sacrificial support configured to support a section of the AM structure during additive manufacturing, wherein the datum structure is coupled to the sacrificial support.

5. The apparatus ofclaim 1, wherein the datum structure includes a first plurality of spaced datum structures on the upper surface of the build platform, each vertical reference plane of the first plurality of datum structures being horizontally coplanar with other vertical reference planes of the rest of the first plurality of spaced datum structures.

6. The apparatus ofclaim 5, wherein the AM structure includes a plurality of AM structures each object thereof including a removal plane extending therein defining a respective lowermost extent of a respective object, wherein at least two of the removal planes are at different distances from the upper surface of the build platform, and

wherein the vertical reference planes of the first plurality of datum structures are horizontally coplanar with the removal planes of the objects of the plurality of AM structures to provide the vertical reference plane for guiding the cutting element to remove each object from a respective remaining portion of a respective AM structure.

7. The apparatus ofclaim 5, wherein the datum structure includes a second plurality of spaced datum structures different than the first plurality of datum structures, each vertical reference plane of the second plurality of datum structures being horizontally coplanar with each vertical reference plane of the rest of the second plurality of spaced datum structures but not horizontally coplanar with the vertical reference planes of the first plurality of datum structures.

8. A method, comprising:

additively manufacturing at least one additive manufacturing (AM) structure on an upper surface of a build platform, the upper surface being at least one of non-horizontal and non-planar, each AM structure including a removal plane extending therein defining an object thereabove; and

while additively manufacturing the at least one AM structure, additively manufacturing at least one datum structure positioned relative to the build platform, each datum structure including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure, wherein each vertical reference plane is horizontally coplanar with the removal plane of each AM structure.

9. The method ofclaim 8, wherein additively manufacturing the at least one datum structure includes additively manufacturing each datum structure directly on the upper surface of the build platform and separated from the at least one AM structure.

10. The method ofclaim 8, wherein additively manufacturing the at least one datum structure includes additively manufacturing each datum structure as part of the at least one AM structure.

11. The method ofclaim 8, wherein additively manufacturing the at least one AM structure includes additively manufacturing a sacrificial support for at least a section of each AM structure, wherein additively manufacturing the at least one datum structure includes additively manufacturing the at least one datum structure operatively coupled to the sacrificial support.

12. The method ofclaim 11, wherein additively manufacturing the at least one datum structure includes additively manufacturing a first plurality of spaced datum structures, each vertical reference plane of the first plurality of datum structures being horizontally coplanar with other vertical reference planes of the rest of the first plurality of spaced datum structures.

13. The method ofclaim 12, wherein additively manufacturing the at least one AM structure includes additively manufacturing a plurality of AM structures, each AM structure including a removal plane extending therein defining an object thereabove, wherein at least two of the removal planes are at different distances from the upper surface of the build platform, and

wherein the vertical reference planes of the first plurality of datum structures are horizontally coplanar with the removal planes of the plurality of AM structures to provide the vertical reference plane for guiding the cutting element to remove the object from the remaining portion of the AM structure.

14. The method ofclaim 12, wherein additively manufacturing the at least one datum structure includes additively manufacturing a second plurality of spaced datum structures different than the first plurality of spaced datum structures, each vertical reference plane of the second plurality of datum structures being horizontally coplanar with each vertical reference plane of the rest of the second plurality of spaced datum structures but not horizontally coplanar with the vertical reference planes of the first plurality of datum structures.

15. The method ofclaim 8 further comprising removing the object from the remaining portion of the AM structure on the upper surface of the build platform using wire electrical discharge machining (w-EDM), the cutting element of the w-EDM passing parallel with each vertical reference plane and through each removal plane of each object.

16. The method ofclaim 8 further comprising:

determining a change in vertical position of the upper surface of the build platform from an expected vertical position of the upper surface at at least one location during the additive manufacturing of the at least one datum structure and the at least one AM structure; and

adjusting the additive manufacturing of the at least one datum structure to ensure the vertical reference plane of the at least one datum structure is horizontally coplanar with the removal plane of the AM structure based on any change in vertical position of the upper surface of the build platform.

17. An additively manufactured (AM) structure, comprising:

a removal plane extending therein defining an object thereabove; and

at least one datum structure coupled relative to the AM structure, the at least one datum structure including a vertical reference plane for guiding a cutting element to remove the object from a remaining portion of the AM structure through the removal plane, the vertical reference plane horizontally coplanar with the removal plane of the object.

18. The AM structure ofclaim 17, wherein a lower surface of the AM structure is not planar.

19. The AM structure ofclaim 17, wherein the at least one datum structure is coupled to the AM structure.

20. The AM structure ofclaim 17, further comprising a sacrificial support configured to support a section of the AM structure during additive manufacturing, and wherein the at least one datum structure is coupled to the sacrificial support.

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